Beechcraft King Air 360 Er vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piper M600 Sls vs Sikorsky S 92
The Beechcraft King Air 360ER and Piper M600 SLS are pressurized fixed‑wing turboprops, while the MD Helicopters (McDonnell Douglas) 902 Explorer and Sikorsky S‑92 are twin‑engine helicopters. In category and mission, the King Air 360ER is a multi‑engine business/utility aircraft optimized for longer trips and flexible cabin layouts; the M600 SLS is a single‑engine personal/business aircraft emphasizing owner‑pilot simplicity; the MD 902 is a light/medium helicopter suited to short‑to‑medium point‑to‑point missions with vertical access; and the S‑92 is a heavy helicopter built for offshore, SAR, and high‑payload transport. On range, the King Air 360ER typically offers the longest legs in this group (roughly 1,500–1,800 nm class depending on payload and reserves). The Piper M600 SLS is also long‑range for its class (about 1,400–1,500 nm). The MD 902 Explorer is shorter range (around 300–400 nm), while the Sikorsky S‑92 is longer among helicopters (about 500–600 nm). For passenger capacity, the M600 SLS typically seats about 5–6, the King Air 360ER commonly carries about 6–9, the MD 902 seats about 7–8, and the S‑92 carries the most, commonly around 19.
| Spec | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 2.19 | $ 19.79 |
| Min Crew | 1 | 2 |
| Total Seats | 6 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Piper | Sikorsky |
| Aircraft Name | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1406 | 439 |
| DOC / nm / Seat | $ 0.55 | $ 0.94 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2200 | 7417 |
| Standard Cabin Seats | 4 | 19 |
| Direct Operating Cost | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 274 | 155 |
| Base Aircraft Price (USD) | $3,081,400 | $30,650,000 |
| Max Cabin Seats | — | 19 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | — |
| Min Crew | 1 | 2 |
| Total Seats | 5 | 21 |
| Galley Location | MID | — |
| Cabin Pressure (psi) | 5.6 | — |
| Galley / Refreshment | Refreshment Centre | — |
| Standard Cabin Seats | 4 | 19 |
| SL Cabin Altitude (ft) | 12600 | — |
| Max Cabin Altitude (ft) | 8644 | — |
| Max Cabin Seats | — | 19 |
| Engine | ||
| FADEC | No | Yes |
| Model | PT6A-42A | CT7-8A |
| TBO (hrs) | 3600 | 4000 |
| Horsepower | 600 | 2520 |
| Flat Rating | ISA + 55 | — |
| No. of Engines | 1 | 1 |
| Fuel Capacity (gal) | 260 | 760 |
| Fuel Type | — | JetFuel |
| Dimensions | ||
| Length (ft) | 29.7 | — |
| Wingspan (ft) | 43.2 | — |
| Cabin Width (ft) | 4.1 | — |
| Cabin Height (ft) | 4 | — |
| Cabin Length (ft) | 12.3 | — |
| Overall Height (ft) | 11.3 | 17.8 |
| Cabin Volume (cu. ft) | 165 | 775 |
| Baggage Volume Int. (cu. ft) | 20 | — |
| Baggage Volume Ext. (cu. ft) | — | 140 |